摘要
变稳飞行控制系统是为我国BW-1纵向变稳飞机研制的控制系统。该系统对飞机实施全权限数字电传操纵,可以在飞行中改变飞机的操纵感觉特性、操纵系统特性和纵向短周期气动特性. 本文介绍该系统可靠性计算及确保飞行安全所采取的措施.
Variable stability FCS is a control system which has been developed for the BW-1 longitudinal variable stability aircraft in China. The system adopts full authority DFBW for aircraft, which may change the characteristics of control feel, handling system and longitudinal short-period aerodynamics during flight.This paper deals with reliability calculation of the system and the measures adopted to ensure flight safety.
出处
《飞行力学》
CSCD
北大核心
1989年第4期64-70,共7页
Flight Dynamics
